Skip to main navigation Skip to search Skip to main content

Adaptive nonsingular fast terminal sliding mode control for spacecraft hovering to noncooperative target

  • Harbin Institute of Technology

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

This paper considers the relative position control of the Line-of-Sight (LOS) based relative motion model, which is highly complicated and strongly coupling nonlinear with the matched disturbance. By employing a novel nonsingular fast terminal sliding mode (NFTSM) surface, the adaptive control law is designed to guarantee the bounded stability of the closed-loop error system without prior knowledge of disturbance bound. Finally, the numerical simulation is presented to show fine performance of the proposed control law.

Original languageEnglish
Title of host publicationProceedings - 2017 Chinese Automation Congress, CAC 2017
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages229-234
Number of pages6
ISBN (Electronic)9781538635247
DOIs
StatePublished - 29 Dec 2017
Event2017 Chinese Automation Congress, CAC 2017 - Jinan, China
Duration: 20 Oct 201722 Oct 2017

Publication series

NameProceedings - 2017 Chinese Automation Congress, CAC 2017
Volume2017-January

Conference

Conference2017 Chinese Automation Congress, CAC 2017
Country/TerritoryChina
CityJinan
Period20/10/1722/10/17

Keywords

  • adaptive control
  • line-of-sight relative motion model
  • nonsingular fast terminal sliding mode
  • spacecraft hovering

Fingerprint

Dive into the research topics of 'Adaptive nonsingular fast terminal sliding mode control for spacecraft hovering to noncooperative target'. Together they form a unique fingerprint.

Cite this